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Airworthiness Directives; General Electric Company CF6-80E1 Series Turbofan Engines

airworthiness · Rule · Final rule; request for comments. · Published 2007-09-11 · Effective 2007-09-26 · 72 FR 51697

Document

Document number
E7-17678
Federal Register citation
72 FR 51697
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
General Electric Company CF6-80E1 Series Turbofan
Publication date
2007-09-11
Effective date
2007-09-26
FAA docket
Docket No. FAA-2007-28726

Abstract

The FAA is adopting a new airworthiness directive (AD) for General Electric Company (GE) CF6-80E1 series turbofan engines with certain part number (P/N) compressor rear frames (CRFs) installed. This AD requires revisions to the Airworthiness Limitations Section (ALS) of the manufacturer's Instructions for Continued Airworthiness (ICA) and air carrier's approved Continued Airworthiness Maintenance Programs (CAMP) to include initial and repetitive eddy current inspections (ECIs) or fluorescent penetrant inspections (FPIs) of the affected CRFs. This AD results from the need to require enhanced inspections of the CF6-80E1 series engine CRFs for cracks. We are issuing this AD to prevent rupture of the CRF, which could result in an under-cowl engine fire.

Source

Authoritative
Federal Register document
Machine
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